SE8005858L - GASSTRALEN PAVERKAD, AUTOMATIC ROBOT DISPENSER WITH POSITIVE RELEASE - Google Patents
GASSTRALEN PAVERKAD, AUTOMATIC ROBOT DISPENSER WITH POSITIVE RELEASEInfo
- Publication number
- SE8005858L SE8005858L SE8005858A SE8005858A SE8005858L SE 8005858 L SE8005858 L SE 8005858L SE 8005858 A SE8005858 A SE 8005858A SE 8005858 A SE8005858 A SE 8005858A SE 8005858 L SE8005858 L SE 8005858L
- Authority
- SE
- Sweden
- Prior art keywords
- rocket
- housing
- lever
- sear
- spring
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41F—APPARATUS FOR LAUNCHING PROJECTILES OR MISSILES FROM BARRELS, e.g. CANNONS; LAUNCHERS FOR ROCKETS OR TORPEDOES; HARPOON GUNS
- F41F3/00—Rocket or torpedo launchers
- F41F3/04—Rocket or torpedo launchers for rockets
- F41F3/052—Means for securing the rocket in the launching apparatus
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Eye Examination Apparatus (AREA)
- Supply Devices, Intensifiers, Converters, And Telemotors (AREA)
- Electrical Discharge Machining, Electrochemical Machining, And Combined Machining (AREA)
Abstract
A missile or rocket detent and positive release mechanism is actuated by the thrustor of a rocket (10). The mechanism is mounted on a housing (42) to which a rocket launcher tube (15) is secured. A spring-loaded lever (50), having a notch (52) and a cam follower (55) at opposite ends, lies parallel to the rocket and is pivoted to the housing. Its notched end extends into the launch tube for positively locking the rocket into place. A spring-loaded sear (62) also lies parallel to the housing, is reciprocable on the launcher, and has a cam (64) which rests against the first lever's follower. At its other end, the sear is pivoted to a toggle (44) lying perpendicular to the housing so that one end (48b) nests against a housing end surface (46) and its other end (48a) extends into the path of the exhaust from the rocket's thrustor. The rocket blast pivots the toggle around on its pivot point against the housing end surface to linearly move the sear and its cam, which pushes against the follower-end of the first lever and pivots the spring-loaded lever sufficiently to withdraw its notched-end from engagement with, and to release the rocket.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US05/974,479 US4336740A (en) | 1978-12-29 | 1978-12-29 | Automatic blast actuated positive release missile detent |
Publications (2)
Publication Number | Publication Date |
---|---|
SE8005858L true SE8005858L (en) | 1980-08-20 |
SE442339B SE442339B (en) | 1985-12-16 |
Family
ID=25522090
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE8005858A SE442339B (en) | 1978-12-29 | 1980-08-20 | ROBOT SHUTTER LOCK ORGANIZATION |
Country Status (10)
Country | Link |
---|---|
US (1) | US4336740A (en) |
KR (2) | KR830001582A (en) |
BE (1) | BE879799A (en) |
CA (1) | CA1153597A (en) |
GB (1) | GB2050583B (en) |
IL (1) | IL58889A (en) |
IT (1) | IT1164799B (en) |
NO (1) | NO147433C (en) |
SE (1) | SE442339B (en) |
WO (1) | WO1980001411A1 (en) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3301567A1 (en) * | 1983-01-19 | 1984-08-02 | Bodenseewerk Gerätetechnik GmbH, 7770 Überlingen | LOCKING DEVICE FOR AIR-AIR STEERING MISSION |
US4545284A (en) * | 1983-04-29 | 1985-10-08 | General Dynamics Pomona Division | Protection device for rocket launcher rail |
US4550640A (en) * | 1983-09-16 | 1985-11-05 | Werkzeugmaschinenfabrik Oerlikon-Buehrle Ag | Missile canister restraint device |
US4734329A (en) * | 1984-05-29 | 1988-03-29 | The United States Of America As Represented By The Secretary Of The Air Force | Shock absorbing missile launch pad |
US4616554A (en) * | 1984-08-13 | 1986-10-14 | Westinghouse Electric Corp. | Extendable tube for vertically delivered weapons |
US4934241A (en) * | 1987-11-12 | 1990-06-19 | General Dynamics Corp. Pomona Division | Rocket exhaust deflector |
US5115711A (en) * | 1991-03-25 | 1992-05-26 | Fmc Corporation | Missile canister and method of fabrication |
US5327809A (en) * | 1993-03-24 | 1994-07-12 | Fmc Corporation | Dual pack canister |
KR0156674B1 (en) * | 1995-12-15 | 1998-10-15 | 배문한 | Missile restraint and removal apparatus |
US6895850B2 (en) | 2003-09-09 | 2005-05-24 | The United States Of America As Represented By The Secretary Of The Navy | Pressure-released brake assembly for restraining projectile in launch tube |
JP4635236B2 (en) * | 2008-10-30 | 2011-02-23 | 独立行政法人産業技術総合研究所 | Manufacturing method of solid-state memory |
US9841256B2 (en) * | 2016-01-17 | 2017-12-12 | Wilcox Industries Corp. | Combined launch and storage tube for missile |
KR102373292B1 (en) * | 2020-08-19 | 2022-03-11 | (주)신화정공 | Apparatus for detention of missiles |
Family Cites Families (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1141210B (en) * | 1959-06-09 | 1962-12-13 | Boelkow Entwicklungen Kg | Launch device for recoil propelled missiles |
FR1340562A (en) * | 1961-12-06 | 1963-10-18 | Brevets Aero Mecaniques | Improvements to rocket launcher installations with launch tubes, in particular those for aerodynes |
NL6411455A (en) * | 1963-10-16 | 1965-04-20 | ||
AT248290B (en) * | 1963-10-16 | 1966-07-25 | Bofors Ab | Device for fastening a projectile in a housing |
US3513749A (en) * | 1968-10-25 | 1970-05-26 | Us Army | Rocket launcher |
US3659493A (en) * | 1970-01-16 | 1972-05-02 | Hitco | Rocket retaining mechanism for launcher tubes |
US3719120A (en) * | 1970-06-29 | 1973-03-06 | Us Navy | Rocket launching system |
CH592861A5 (en) * | 1975-10-03 | 1977-11-15 | Oerlikon Buehrle Ag | Clamp holding rocket in launching barrel - has locking lever releasing clamp by rocket gas stream force |
US4132150A (en) * | 1977-08-08 | 1979-01-02 | The Unites States Of America As Represented By The Secretary Of The Army | Blast actuated detent |
-
1978
- 1978-12-29 US US05/974,479 patent/US4336740A/en not_active Expired - Lifetime
-
1979
- 1979-10-23 CA CA000338177A patent/CA1153597A/en not_active Expired
- 1979-11-05 BE BE2/58182A patent/BE879799A/en not_active IP Right Cessation
- 1979-12-06 IL IL58889A patent/IL58889A/en not_active IP Right Cessation
- 1979-12-26 WO PCT/US1979/001122 patent/WO1980001411A1/en unknown
- 1979-12-26 GB GB8027583A patent/GB2050583B/en not_active Expired
- 1979-12-28 IT IT51221/79A patent/IT1164799B/en active
- 1979-12-28 KR KR1019790004656A patent/KR830001582A/en unknown
- 1979-12-28 NO NO794350A patent/NO147433C/en unknown
-
1980
- 1980-08-20 SE SE8005858A patent/SE442339B/en unknown
-
1983
- 1983-06-01 KR KR2019830004833U patent/KR830001147Y1/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
NO147433B (en) | 1982-12-27 |
IT7951221A0 (en) | 1979-12-28 |
GB2050583B (en) | 1983-03-30 |
CA1153597A (en) | 1983-09-13 |
GB2050583A (en) | 1981-01-07 |
WO1980001411A1 (en) | 1980-07-10 |
KR830001147Y1 (en) | 1983-07-13 |
KR830001582A (en) | 1983-05-17 |
NO147433C (en) | 1983-04-06 |
IT1164799B (en) | 1987-04-15 |
NO794350L (en) | 1980-07-01 |
SE442339B (en) | 1985-12-16 |
US4336740A (en) | 1982-06-29 |
BE879799A (en) | 1980-03-03 |
IL58889A (en) | 1982-04-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
NAL | Patent in force |
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